The Quantum Efficiency of the Mercury Sensitized Photochemical

sized and their mass spectra determined on a Nier type and a Consolidated mass spectrometer. A method of calculating the mass spectrum. 2. [CONTRIBUTI...
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Aug., 1948

PHOTOCHEMICAL DECOMPOSITION OF HYDROGEN

Conclusion 1. Monodeuteromethane, tetradeuteromethane. monodeuteroethane, monodeuteropropane-1 and monodeuteropropane-2 have been synthesized and their mass spectra determined on a Nier type and a Consolidated mass spectrometer. 2. A method of calculating the mass spectrum

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of monodeuteromethane and monodeuteroethane from the ConesPonding light hydrogen cornPounds, has been hdicated. 3. A method has been given to indicate the position of a deuterium atom in monodeuteropropanes. RECEIVED JANUARY 27, 1948

[CONTRIBUTION FROM CHEMICAL LABORATORY, UNIVERSITY OF MISSOURI]

The Quantum Efficiency of the Mercury Sensitized Photochemical Decomposition of Hydrogen BY LLOYD B. THOMAS AND WM. D. GWINN'~ Introduction The reaction between mercury atoms excited by absorption of light of X 2537 A. and hydrogen molecules to produce hydrogen atoms was reported by Cario and Franck' in 1922. The analogous reaction between hydrogen molecules and mercury atoms excited by streaming electrons of controlled energy through the gas mixture has been carried out.2 These and more recent studies in this laboratory have indicated that the 6*P, state of mercury to which the photochemical reaction is ascribed may play only a slight part, if any, in the electron initiated reaction. The immediate occasion for undertaking the present study is to obtain the necessary reaction rate data to compare the kinetics of the electron and photon activated reactions in the hope that the mechanism of the former will be clarified. Attention has been devoted by a number of investigatordtuart, Zemansky, Bates3 and E v a n s e t o the quenching of fluorescent resonance radiation from Hg3P1atoms by collision of the Hg3P1atoms with added foreign gas molecules. An over-all effective cross section for quenching is obtained through the method but it is not possible to distinguish between processes which may contribute to the quenching. By the method of the present paper it appears possible to determine the effective cross section for a specific process, Le., the interaction of Hg3P1 atoms with hydrogen molecules to cause their removal from the gas phase, presumably through dissociation. Experimental The reaction systein and light source are shdwn in Fig. 1. The reaction cell is a cylinder of fused silica which has an internal length of 3.53 cm. and an internal diameter of 2.25 cm. The walls of the cell are lined with a thin cylinder of oxidized copper. The ends of the cylinder are flat polished fused silica windows 2 mm. thick and are (la) Present address of W. D. G. is Department of Chemistry, University of California, Berkeley, Calif. (1) Cario and Franck, 2. Phyrik, 11, 155 (1922). (2) Glockler and Thomas, THIS JOURNAL, 61, 2352 (1936). (3) A. C. G. Mitchell and M. W. Zemansky, "Resonance Radiation and Excited Atoms," Cambridge University Press, 1934. (4) Evans, J . Chrm. Phys., 1,445 (1934).

fused on. The cell is attached to the rest of the system, which is of Pyrex, by a graded seal. The Pirani gage consists of a 0.0025 cm. platinum filament mounted as shown and immersed in kerosene filled thermostat which is maintained at 30 Precaution was taken to prevent a film of kerosene, which was found t o absorb A-2537, from creeping over the entrance window. The system in the thermostat was connected through a Utube and mercury cut-off t o a conventional high vacuum system with mercury condensation pump, McLeod gage, mercury cut-offs, and with no stopcocks in the high vacuum line. Hydrogen was admitted from a gas flame through a palladium tube. The pressure was brought to the desired values, as shown by the McLeod gage, through manipulation of the flame and cut-offs.

.

,--RESONANCE

LAMP

HOUSING

SHUTTER

u

c /

REACTION

LLRO3ENi

t Fig. 1.-Experimental

apparatus.

The light source is a monochromatic resonance lamps which operates several degrees above room tern erature and gives a very narrow line breadth-about ZOggreater than the Doppler breadth at 30". A fused silica photoelectric cell with a cadmiun coated cathode was mounted above the resonance lamp as shown and served as a check on the lamp intensity. The intensity of A 2537 in this upper position was strictly proportional t o that a t the reaction cell window when the mercury vapor pressure in the resonance lamp cylinder was kept constant. The procedure in taking data is as follows: The thermostat is replaced by an oven. Oxygen is admitted to the system t o about 10 mm. pressure. When the oven temperature becomes sufficiently high the oxygen pressure starts to diminish due to consumption by the copper of (6) Thomas, Rev. Sci. Inst., 12, 809 (1941).

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LLOYDB. THOMAS AND WM. D. GWINN

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the cylinder. After the oxygen pressure has diminished about 1 mm. the oxygen is pumped out and the system is baked and flamed while open t o the pumps. The thermostat is then replaced, the temperature of a mercury droplet introduced to the U-tube is set at the desired value, hydrogen is introduced t o the desired pressure, and the cut-off t o the reaction system is closed. After bringing the Pirani gage t o balance and bringing the lamp t o a steady intensity, the foot-operated shutter below the resqnance lamp is opened for a measured time interval. This interval is regulated from four to sixty seconds, depending on the pressures of hydrogen and mercury vapor in the system, t o give a Pirani galvanometer excursion of from 10 t o 30 scale divisions (readable t o 0.1 division), which corresponds t o the disappearance of less than gram of hydrogen. After about five such average exposures the baking-out procedure is repeated. This is necessary because it was found that the observed rates of decomposition began to decrease measurably with total decomposition in excess of this amount. This effect seems t o be attributable to the inability of the silica surface t o maintain its full capacity for removal of the products of the reaction. All of the data reported in this paper were taken in the initial period after baking out and forming a fresh oxide surface when the reaction rates at a given set of concentration and radiation conditions were quite constant and at a maximum. The lamp intensity was determined by use of two multiple junction bismuth-silver vacuum thermopiles, one bismuth-(bismuth, 5% tin) vacuum thermopile, two quartzcadmium photocells, the chloroacetic acid actinometer, and two N.B .S. calibrated lamps along lines described .earlier.* Ten sets of determinations of the resonance lamp intensity gave 25.6 X 1012 quanta entering the reaction vessel per second for unit (upper position) photocell galvanometer deflection. The absorption (including reflection) of light from the resonance lamp and N.B.S.standard lamps in thermopile and reaction cell windows was measured and the proper corrections were made. As a check on the reliability of the lamp standardization the quantum yield of the chloroacetic acid hydrolysis was run. A quantum yield of 0.29 at 26" was found, which is t o be compared with the value 0.33 obtained by Smith, Leighton and highton.' (The value of 0.342 previously given by Thomasd should be revised to 0.29 when correction is allowed for absorption of the radiation of the N.B.S. lamps in the two mm. fused silica ground and polished windows of the thermopiles.) The absorption for the resonance lamp by the mercury vapor in the reaction cell was calculated from measurements made in a cell similar t o the reaction cell but of better optical quality and described with equations used in reference 5. The value of w (ref. 5 , p. 311) was found

t o be approximately 1.2 and the integral expression with this value of w and the "1" for the reaction cell of Fig. 1 was used to calculate the absorption in the reaction cell at the various pressures of mercury vapor. This absorption, multiplied by the number of quanta entering the cell per second per unit photocell galvanometer deflection, is plotted in Fig. 2, Curve A.

The Experimental Data The measurements were made a t three hydrogen pressures, 0.02, 0.05 and 0.lr mm. over a range of mercury vapor pressures from 0.3 X to 30 X mm. These data, expressed in hydrogen molecules disappearing per second per unit photocell galvanometer deflection (photocell mounted above resonance lamp), are shown plotted against the pressure of mercury vapor in Fig. 2, Curves H, C, D. Most of the points shown in these curves represent an aggregate of several points so closely placed that they could not be plotted distinctly on a graph of this scale. The data considered in determining the curves are given below in Table I under the column headings I and 11, representing, respectively, the mercury vapor pressure in mm. X lo4 and the rate of removal of hydrogen in molecules per second per unit photocell galvanometer current X lo-'*. The number of separate measurements taken to obtain the average value given is indicated by the numbers in parentheses in case of more than one. Column I11 lists the quanta of X 2537 ( X absorbed in the cell per second per unit photocell current over the range of mercury vapor pressures. These are plotted in Curve A, Fig. 2. TABLE I REACTIONRATEhf RASLXEMENTS A K D LIGHTABSORPTION I N THE CELL

I, Pressure of Mercury Vapor ( X lo*). 11, Hydrogen molecules renioved per second per unit photocell current ( X 10-13). 111, Quanta of X-3537 absorbed within cell per second per unit photocell current ( X 10-13). 0.11 I 0.3 1.85 2.95 5.8 5.9 6.2 8.7 8.9 9.0 9.6 16.1 19.16 28.8

mm. Hr

0.06 mm. HI 0.02 mm. Hr I1 I I1 I I1 I 1.83 0 . 7 0 (3) 1 . 8 6 0.303 (3) 0 . 0 0.277 1.85 0.694 (3) 1.85 0 . 3 (3) 1.0 1.2215) 1.53 (2) 5 . 8 1.42 (2) 6 . 0 0 . 8 3 (3) 2.0 5 . 9 1.54 (3) 6 . 1 0.848 4.0 2.37 (3) 7 . 9 5 0.945 (3) 8 . 0 2.415 (2) 7 . 0 5 1.65 (3) 2.62 9 . 9 3.14 1 3 . 5 1 . 4 4 ( 2 ) 16.0 2.86 14.05 2.60 (3) 19.8 1.91 (2) 2 4 . 0 19.15 3 . 0 2 (2) 19.95 1.87 (2) 2.97 27.7 3 . 1 5 ( 2 ) 2L.6 2.01 3.12 27.7 3 . 2 0 3.10 5.78(3)

I11

0.0 14.3 18.5 22.8 24.5 25.1 26.4

4.3 4.65 (3)

Discussion

0

4 8 1 2 1 6 2 0 2 4 2 8 Pressure of mercury vapor ( X 104). Fig. 2.-Experimentd data.

L. B. Thomas, Tars JOURNAL, (IS,1879 (1940). (7) Smith, Leighton and Leighton,iMd.. 61, 2299 (1939). (6)

To express the data in more significant forin, curves were put through the experimental points (Curves B, C, and D of Fig. 2) and the ordinates of these curves were divided respectively by the ordinates of Curve A, Fig. 2 a t corresponding abscissas. The resulting values are plotted in Fig. 3 for each of the hydrogen pressures investigated. The ordinates of these curves are the quantum efficiencies at the various mercury vapor

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PHOTOCHEMICAL DECOMPOSITION OF HYDROGEN

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pressures. It is seeii that the quantum efficiency given earlier by Zeman~ky.~The value 2.5 X cm.2 is selected for u2 for the process resultrises markedly over the mercury pressure rangemore than eight-fold a t 0.02 mm. hydrogen and 4 ing in disappearance of hydrogen from the interfold a t 0.11 mm. hydrogen pressure. A t the pres- cept measurements. sure conditions of these experiments the chance that the Hg3P1atoms will radiate is much greater than the chance that they will be quenched. The increasing quantum yield with increasing mercury pressure i’s due no doubt to the increasing reabsorption of fluorescent X 2537 within the reaction cell. One of the problems of this paper is to give a quantitative statement of the contribution of this reabsorption process to the reaction kinetics. The curves of Fig. 3 permit quite definite extrapolation to the axis of zero mercury vapor pressure. The limiting values of the quantum efficiencies a t zero mercury vapor pressure are 0 4 8 12 16 20 24 28 0.0095 a t 0.02 mm. of hydrogen; 0.023 a t 0.05 Pressure of mercury vapor ( X lo4). mm. of hydrogen; and 0.045 at 0.11 mm. of hyFig. 3.-Quantum efficiency. drogen. These extrapolated values should give the probabilities that single mercury atoms exA series of reactions which constitutes the mechcited to the 8P1 state will react with hydrogen anism will be postulated and on the basis of this molecules a t the specified pressures to cause disappearance of the hydrogen from the gas phase mechanism the rate constants and the contribuand they should be free from complications result- tion of the reabsorption of fluorescent radiation to ing from reabsorption of the fluorescent quanta. the reaction rates will be determined. The reThey may be used to calculate the effective cross actions postulated are: 1, absorption of X 2537 section for the process through use of the collision quanta by the mercury atoms in the gas mixture; frequency expression: 2 = 5.64 X 106nnHr*nHg*-f 2, fluorescence of X 2537 quanta followed by partial (for hydrogen and mercury a t 30’) in which u2 is reabsorption to an extent depending on the meroften termed the “effective cross section” for the cury atom concentration; 3, reaction of HgaPl given p r o c e ~ s . ~To apply the present case con- atoms resulting in dissociation of hydrogen; sider the absorption of one quantum per cc. per 4, collision of Hg3P1atoms and hydrogen resulting second. Then the number of effective collisions in quenching of the Hg3P1atoms but’not resulting per cc. per second, 2, becomes the quantum effi- in dissociation of hydrogen. These processes may ciency, q5, and the nHg* becomes the product of 7, be written as the average life of the Hg3Pl state (1.07 X lo-’ (1) Hgl& + hv (A 2537) +Hg’Pl sec.), and (1 - 4). Substitution of the approhv (A 2537) (2) HgaP1+Hgl& priate values in (1) gives for the intercept with Hz +Hgl& + 2H K. E. (3) HgaPi 0.02 mm. of hydrogen : Hz +Hgl& HZ+ K. E. (4) HgsPi 0.0095 = 5.64 X lo6 X 6.42 X 1014 X 1.07 X lo-’ The removal of Hg3Pl atoms by Process (2) (1 - 0.0095)~~ is greatly modified by reabsorption by the Hgl& From this, u2 = 2.45 X 10-lfi cm.2a t 0.02 mm..of atoms. It is desired that Prqcess ( 2 ) represent hydrogen. Similarly u2 is found to be 2.43 X the net fluorescence, ie., only those quanta that 10-le and 2.21 X a t 0.05 mm. and 0.11 mm. leave the reacting mixture should be counted as of hydrogen, respectively. I t appears likely that fluorescence. The remainder of the quanta are other quenching processes are competing with that supplied for repetition of Process (1). It is seen resulting in disappearance of hydrogen. The from superficial examination of Fig. 3 that the over-all cross section for quenching of Hg3P1 number of quanta supplied for Process (1) by atoms by hydrogen is variously given from 27 to Process (2) may be of the order of eight times as 6.01 X cma2by several investigator^.^,^ great as that supplied directly from the lamp. The last value of Zemansky,aconfirmed by Evans4 The velocity constant for Process (2) is simply the using the same apparatus and theory, should be Einstein “A” coefficient or the reciprocal of the most reliable. The 4 value used in the ~ ( 1 I#) mean life, 7, of the 63P1 state, and this will be term to calculate n ~ should ~ * refer to total quench- modified to represent the net fluorescence by muling rather than to dissociation of hydrogen. In tiplying by a factor which will be designated F calculating the u2 values below, the I$ in (1 - I#) (Hg’So). This function of the concentration of is multiplied by the ratio of the u2 for quenching Hg’So, i.e., F (HglSo), will have the characteristic (uQ~)to the u2 for dissociation of hydrogen (uD’). that it approaches unity as the concentration of This gives U D values ~ 2.50, 2.50 and 2.37 X Hg’So atoms approaches zero, and it tends toward cm.2for U Q ~= 6.01 X 10-lfi cm.2,or 2.53, 2.57 and zero as (HgISo) becomes large. F(Hg’S0) may be 2.51 X 10-lfi cm.‘ for an2 = 8.6 X cm.* defined as the mean probability that a quantum

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of fluorescent radiation will escape reabsorption within the reaction system. It is of course a function of the size and shape of the reaction vessel as well as the mercury vapor pressure. Reaction (3) represents the main feature of the Cario and Franck reaction, ;.e., a collision of the second kind with utilization of the energy of excitation of mercury atoms to supply the energy of dissociation of hydrogen. It appears necessary to postulate reaction (4) to take into consideration the above-mentionedvariance of U Q and ~ U D ~ and , to develop a proper overall kinetic expression to fit the data. Reaction (4) represents a process unspecified as to detail whereby mercury atoms lose their excitational energy a t a rate proportional to the hydrogen pressure but the process does not result in a pressure decrease as would be expected if dissociation occurred. This proposed process would contribute to the over-all kinetics in somewhat the same manner as would failure of the apparatus to achieve complete clean-up of the H atoms by a factor proportional to the hydrogen pressure but this, as is discussed later, is not thought to be the case. Reaction (4) would, superficially a t least, be considered improbable because of the larger (than reaction (3)) amount of kinetic energy developed. However, if the hydrogen molecule comes out of the collision in a high vibrational state, this kinetic energy term would not necessarily be much larger than the 0.3 e.v. of reaction (3). One can write many other reactions which conceivably could occur under the conditions of this experiment. There is no doubt some production of Hg3Pometastable atoms from collision of Hg3P1 atoms with HglSo atoms or hydrogen molecules. The possibility was considered that the equivalent of reaction (4)might occur through conversion of Hg3P1 atoms to Hg3Po atoms by collision with hydrogen if the HgaPo atoms were unable to react efficiently with hydrogen to give a pressure decrease. The results of Meyera (which we have confirmed with monochromatic X 2537) indicate that the Hg8Po atoms can react with hydrogen. The effective cross section for the reaction may be quite low and still give the observed augmented reaction rate with nitrogen added because, with the great excess of nitrogen used, the diffusion time of the Hg3Po atoms (formed by collision of Hg3Pl atoms with nitrogen) to the wall would allow a great many collisions with hydrogen. At the pressure conditions of the present work the Hg3Po atoms would mostly reach the wall (if the Hg3P,-H2 cross section were low). However, against this mechanism for reaction (4) is the fact that the first vibrational quantum of hydrogen is approximately 0.5 e.v. which leads one to expect low probability of conversion of Hg3P1 to Hg3Po atoms which involves only 0.218 e.v.(see ref. (4), p. 450, or ref. (3), p. 225). ( 8 ) hleycr. E . Physik 37, 630 (1026).

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On the basis of Reactions (1) to (4) one obtains an expression for the rate R = -d(Hz)/dt in terms of the constants, concentrations, and Io, which is the number of quanta absorbed per (cc. X sec.). Noting that the quantum yield, (b = R/Ia, one obtains the expression : 1 - 3

4

koF(Hg'So) I ka

ka(Hd

+ kd kr

If the postulated mechanism fits the reaction, the data of Fig. 3 plotted as l/+ os. l/(Hz) should give straight lines with slopes k2F(Hg1So)/kaand a common intercept of (k3 k 4 ) / k 3 . Figure 4 shows the data a t the three hydrogen pressures plotted for seven values of pressure of mercury vapor. It is seen that the plots do give quite closely a family of straight lines with a common intercept. The intercepts lie between 4.0 and 5.5 with an average about 4.5 for 1/+. Since Curve A, Fig. 4, is for (Hg'So) = 0, the value of F(HglS0) is unity and the slope of this curve, 1.96, is the ratio k2/ka. The value of kz is the Einstein "A" coefficient for the transition 63P1---f 6lSo and has the value 1 / ~= 1/1.07 X lo-', hence ka = 1/1.07 X lo-' X 1.96 = 4.77 X lo6. This is the velocity constant for the reaction (3) in the postulated mechanism and this work constitutes, so far as we are aware, the only attempt a t its measurement for this classic reaction. The above constant gives the rate a t 30' in molecules of hydrogen per cc. decomposed per second per millimeter of hydrogen pressure per unit concentration of Hg3P1atoms in atoms/cc. If the hydrogen concentration is expressed in molecules per cc. instead of millimeters of pressure, k3 becomes 4.77 X 106/3.20 X 10l6 = 1.49 X 10-lo. It is of interest to calculate the collision cross section from this constant and to compare with the result obtained previously. In the collision frequency expression Z may be set equal to ka when TZH, = 1 and nHg* = 1. The value of u2 is found to be 2.64 X as against 2.50 X 10-l6 found from consideration of the intercepts of Fig. 3 and published values of U Q ~ . It has been pointed out that the intercepts of the lines on Fig. 4 on the 1/+ axis average about 4.5 which is, according to the postulated mechanism, (k3 k4)/k3. The value of h / k 3 is 3.5 and kq = 3.5 X 1~49X 10-lo = 5.22 X 10-lo. One would expect so far as the extrapolation to infinite hydrogen pressure, i.e., l/(H*) = 0, is valid that the intercept value, 4.5, would agree with the U Q ~ / U Dratio. ~ It is larger than the ratios obtained using either of the values previously mentioned (8.6 and 6.01 X cm.2) and U D ~(2.64 X 10-l6) which give 3.3 and 2.3, respectively. Larger values of have been reported but are considered less reliable.3 This discrepancy, if real, is perhaps explainable on the assumption of a collision-induced emission of X 2537 (by hydrogen on Hg3P1atoms) with the line sufficiently broadened to allow these quanta to escape reabsorption. These quanta would be quenched from the stand-

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PHOTOCHEMICAL DECOMPOSITION OF HYDROGEN

L

o 0000

MY YO

w o n

2 1.0 F

EXPERIMENTAL

@

- 6 - 5

2 0.8 8 0.6 g2 0.4

- 4

v

h

M

CALCULATED

C

i?

00012

P.9

E 3 9 1 9

E

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6o

t

/

-3

40

0.2

20

I I I I I I 0.0 0 4 8 12 16 20 24 Pressure of mercury vapor (mm. X 104). Fig. 5.

20 30 l/pressure of hydrogen Fig. 4. 10

40

50

point of the present experiment but would show up as fluorescence in the quenching studies. The ratios of the slopes of the lower lines of Fig. 4 to that of the upper line (A), for which F(HglSo) is unity, are the values for F(Hg’So) for the various pressures of mercury vapor. These values are plotted in Fig. 5, Curve A. The ordinates of this curve are the probabilities, for the mercury vapor pressures in the particular vessel used, that a quantum of X 2537 emitted as fluorescent radiation will escape reabsorption within the bounds of the vessel. The quantity [l - F(Hg’So)] is then the probability that the fluorescent quantum will be reabsorbed, and, since the time spent by a quantum of energy as radiation is negligible compared to r , the same quantity may be interpreted as the fraction of the quanta of energy, present in the system with the light source on, which are still present at the time, 7 , after the light source is cut off. Also [l - F(HglSo)1” is the fraction of quanta still in the system after n ~ .This leads to an exponential decay function for the intensity of radiation emitted after excitation is cut off and we may write approximately It/lo = [l - F (Hg’So)]” = e-@ in which t = nr. The values of p calculated from F(Hg’So) are shown in Fig. 5, Curve C. It is possible to estimate P theoretically through a series of methods due to Milne, Zemansky, Samson, Kenty, summarized in reference (3), p. 228 et seq. It is necessary to consider a distance, 1, through which the radiation must diffuse which we have estimated as 1.125 cm., the radius of the reaction, vessel. The values of p so calculated are shown in Curve B, Fig. 5. The experimental values from F(Hgl&) deviate an average of 10% from the calculated values over the range of mercury vapor pressures shown. The agreement is of about the same order as that obtained by comparison of direct measurements of /3 with the calcu-

lated value^.^ Such close agreement must be regarded as fortuitous but the fact that it was possible to arrive, through treatment of the data of this paper, a t the F(Hg’S0) values which are consistent with existing theory and experiment applied to the “imprisonment” of resonance radiation in the strictly physical (not chemicallyreacting) system, mercury vapor, seems to support the essential validity of the data and its treatment. We have carried through an application of Milne’s theory of the diffusion of “imprisoned” resonance radiation to calculate the number of Hg3P1atoms present in the system and thence the rate of disappearance of hydrogen, i. e., Curve B, C, D, Fig. 2. The expression for the rate involves two effective cross sections, one for reaction (3) of this paper and the other for over-all quenching of Hg3P1atoms by Hz. It is found that rate curves of the general characteristics of B, C, D, Fig. 2 are obtained and that quantitative agreement with experiment is much better if the U D and ~ U Q values ~ 2.5 X from this work and 8.6 X cme2from ref. (3) both are used than if either valye is used as the sole cross section involved, The question arose in conversation with J. Franck as to the possibility that these experiments might be used to distinguish between the two proposed mechanisms involving direct dissociation of hydrogen molecules as against formation of mercury hydride in the process. If one assumes that the hydrogen in the mercury hydride is not cleaned up and is eventually returned as hydrogen to the gas and if one assumes that no other quenching processes than one of the two proposed are involved, a study of the quenching externally and hydrogen removal internally should be able to distinguish between the two mechanisms. One quantum per hydrogen molecule disappearing would be quenched in the first case and two quanta in the second case. Quenching measurements have been made giving an estimated quenching, averaged over the surface of a sphere concentric with and about the cylinder, of

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LLOYD B. THOMAS AND WM.D. GWINN

3.5 times the quantum yield observed internally. This is again a measure of U Q ~ / U Dand ~ constitutes further confirmation that one or more other quenching processes than that resulting in hydrogen removal is in preponderance. It seems doubtful then that the two mechanisms can be distinguished by this means. An important assumption upon which the validity of much of the interpretation of the data of this paper rests is that the cleanup of the supposed atomic hydrogen produced is complete. This would be a very difficult assumption to demonstrate conclusively by experiment but we have little doubt of its validity because of the evidence presented below. As mentioned in the Experimental section of this paper, all of the data presented were taken a t the limiting condition of maximum rate following reoxidation of the copper and thorough outgassing of the vessel. The reproducibility and consistency of the data is in itself strong evidence of the essential cornpleteness of the cleanup. It would be difficult to imagine a kind of adsorption process a t the silicon dioxide and cupric oxide surfaces which consistently returned a constant fraction of the reaction products as hydrogen to the gas phase. The following experiment substantiates the assumption of complete clean-up. The reaction was carried out in a fused silica cell without any cupric oxide in it. The rate of reaction as observed on the Pirani gage under constant conditions (except for the inside walls) falls gradually to zero when the walls can no longer remove the products and complete recombination of hydrogen atoms then occurs. The rate becomes practically zero when amounts of hydrogen of the order of 100-fold those used in taking the data of this paper were consumed. When the reaction cell with its cupric oxide lining cylinder is used in a similar attempt to exhaust the capacity for removal of the reaction products it is found that the rate falls off less rapidly than ia the former case and becomes flat a t a fraction of the initial rate which agrees to within a few per cent. with the fraction of the internal area of the vessel which consists of cupric oxide. (These experiments were carried out with the mercury vapor pressure low in order to spread the reaction more uniformly through the vessel.) (One might be tempted to attribute the sustained behavior with cupric oxide to the steady conversion of hydrogen to water, hence due to the smaller heat conductivity of water, the Pirani gage would show a pressure decrease. However, the accommodation coefficients and CV values of hydrogen and water gre such that in the “free molecule” heat conduction range here applicable, water is 40% more effective than hydrogen in heat conduction from bright p l a t i n ~ m . ~ The ) interpretation then that we place on the above experi(9) Thomas and Olmer, Tms JOURNAL, 66, 1036 (19431.

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ments is that both silicon dioxide and cupric oxide have the same initial efficiencies of removal of the reaction products and this is very unlikely unless both efficiencies are unity. That cupric oxide has sustained, constant efficiency is found in the extensive work done in this laboratory with the electron initiated mercury sensitized decomposition of hydrogen in which the reaction region is more completely surrounded with oxidized copper surface and the initial rates are maintained longer than with the silica, copper oxide cell. The electron work shows constancy of clean-up efficiency with varying reaction rate and with varying mercury pressure, complete quantitative reproducibility of data, and is entirely consistent with the assumption of complete clean-up efficiency. Lastly, mentioned in connection with completeness of cleanup and general validity of the quantum yield measurements, an independent check was made of four points on Fig. 3. A new vacuum and gas handling system, new Pirani gage and electrical measuring system with new calibrations, new reaction cell with reaction volume more completely surrounded with cupric oxide, and a new photocell were used and the uranyl sulfateoxalic acid actinometer, following the specifications and general procedures of Leighton and Forbes, was used to determine the lamp intensity. The quantum yields a t each hydrogen pressure with mercury a t 0’ and with hydrogen a t 0.11 mm. and mercury at 24’ $ere determined. The four new values of 4 averaged 1.5y0(of @) higher than the four original values with a maximum discrepancy of 5.5y0,i. e., a Q of 0.036 became 0.038 in the new determination. Summary The quantum efficiency of the Cario and Franck mercury sensitized decomposition of hydrogen with A 2537 has been investigated as a function of mercury and hydrogen pressures. On the basis of the postulated mechanism the velocity constant and the effective cross section are determined for the interaction of Hg3P1 atoms and hydrogen resulting in disappearance of hydrogen from the gas phase, presumably through dissociation and removal of the resulting hydrogen atoms on cupric oxide or silicon dioxide walls. The contribution of the reabsorption of fluorescent radiation to the efficiency is singled out and from this the time decay constant of A 2537 from pure mercury vapor in the reaction vessel after excitation is cut off is calculated and compaied with physical theory and measurement. The evidence from several aspects indicates consistently that other quenching processes than that resulting in removal of hydrogen are effective and that the rate of quenching of HgVl atom is several times as great as the rate of removal of hydrogen from the gas. COLUMBIA, MISSOURI

RECEIVED MARCH 6, 1948